2018
DOI: 10.1063/1.5028209
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The effect of surface roughness on rotor-stator cavity flows

Abstract: We are concerned with the CFD simulation of annular rotor-stator cavities using the general purpose second-order finite volume method (FVM) solver OpenFOAM ® and Large Eddy Simulation (LES) methods. Simulations of cavities with smooth surfaces are conducted at various Reynolds numbers, and the properties of the mean turbulent flows are validated against experimental and numerical data available in the literature. Comparisons show that second-order accurate FVM approaches can produce high-fidelity simulations o… Show more

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Cited by 9 publications
(2 citation statements)
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References 47 publications
(68 reference statements)
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“…Fernando et al used the general-purpose second-order finite volume method (FVM) solver and LES to conduct simulations of cavities with smooth surfaces at various Reynolds numbers. Then the properties of the mean turbulent flows are validated against experimental and numerical data available in the literature (Fernando et al, 2018). Bu et al (2017) provided a detailed explanation of flow transport between rotor and stator, which was not reported before.…”
Section: Analysis Of Thermal Flow Fieldmentioning
confidence: 99%
“…Fernando et al used the general-purpose second-order finite volume method (FVM) solver and LES to conduct simulations of cavities with smooth surfaces at various Reynolds numbers. Then the properties of the mean turbulent flows are validated against experimental and numerical data available in the literature (Fernando et al, 2018). Bu et al (2017) provided a detailed explanation of flow transport between rotor and stator, which was not reported before.…”
Section: Analysis Of Thermal Flow Fieldmentioning
confidence: 99%
“…Bridel-Bertomeu 62 components. Moreover, our recent publication 63 visualised the development of instability patterns on the rotor boundary layer of an identical rotor-stator cavity using a vortex identification method, 64 and the outcomes at Re ω = 1 × 10 5 have been compared with a higher Reynolds number case of Re ω = 4 × 10 5 . Figure 9 shows radial and tangential turbulence intensity profiles at r * = 0.50 for different volume fractions.…”
Section: B Single-phase Simulations Of Rotor-stator Nanofluidsmentioning
confidence: 99%